BAI73
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November 2015 edit
Hello, BAI73. We welcome your contributions, but if you have an external relationship with some of the people, places or things you have written about in the article BDC Aero Puma, you may have a conflict of interest. People with a conflict of interest may be unduly influenced by their connection to the topic. For information on how to contribute to Wikipedia when you have a conflict of interest, see the conflict of interest guideline and frequently asked questions for organizations. In particular, please:
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Please familiarize yourself with relevant policies and guidelines, especially those pertaining to neutral point of view, sourcing, and autobiographies. Thank you. Ahunt (talk) 22:48, 2 November 2015 (UTC)
Hello, BAI73. We welcome your contributions, but if you have an external relationship with some of the people, places or things you have written about in the article BDC Aero Industrie, you may have a conflict of interest. People with a conflict of interest may be unduly influenced by their connection to the topic. For information on how to contribute to Wikipedia when you have a conflict of interest, see the conflict of interest guideline and frequently asked questions for organizations. In particular, please:
- avoid editing or creating articles related to you, your organization, its competitors, or projects and products you or they are involved with;
- instead, propose changes on the talk pages of affected articles (see the
{{request edit}}template); - avoid linking to the Wikipedia article or website of your organization in other articles (see WP:SPAM);
- exercise great caution so that you do not violate Wikipedia's content policies.
In addition, the Wikimedia Foundation's terms of use require disclosure of your employer, client, and affiliation with respect to any contribution for which you receive, or expect to receive, compensation.
Please familiarize yourself with relevant policies and guidelines, especially those pertaining to neutral point of view, sourcing, and autobiographies. Thank you. Ahunt (talk) 22:52, 2 November 2015 (UTC)
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General article correction for BDC Aero Industrie Inc and Puma AIrcraft. edit
Correction #1 Under the title BDC Aero Industrie Inc. is a Canadian aircraft manufacturer based in Lachute, Quebec founded in 2008. The company specializes in the production of aircraft ready-to-fly under the following categories: For Canada Advanced Ultralight Aircraft and Limited Class with Special Certificate of Airworthiness For USA light-sport aircraft category references are from Government of Canada and transport Canada
correction #2 Products The company's sole design is the Puma Advanced Ultralight, Puma Sport, Puma LSA, all single engine References are on the website, Transport Canada, BAI73 (talk) 01:16, 3 November 2015 (UTC)
For the aircraft this is the corrected information
Correction #1 The title BDC Aero Puma does not exist, BDC Aero Industrie Inc. is a company Puma is one of the product so the title should be Puma Aircraft References are on the Government of Canada
Correction #2 Under the title The Puma Aircraft is a Canadian aircraft, originally designed and named Pluto by the Italian designer Antonio Bortolanza in the mid-1980s designed according to the European standard under ultralight regulation to meet the max takeoff weight of 990lbs. In 2008 BDC Aero Industrie Inc. redesign the aircraft size, structure, and make a systematic production procedure with quality control system to fit the North American market requirements for Canada and USA.Although the airplane resemble the Italian made, the new PUMA, has a complete new structure, components, interior, and it is engineered to have a max gross weight of 1320 lbs and 1420 lbs on floats. The Puma is equipped with Rotax 912 UL, 912ULS, 912iS, 914UL engines. The aircraft is only sold as factory build under three different categories: Light Sport Aircraft (U.S.A only) VFR day/night Experimental (U.S.A only) VFR day/night, IFR Limited Class (Canada and other countries) VFR day/night, IFR Advanced UltraLight (Canada) VFR day only At the moment BDC Aero Industrie do not offer home build amateur construction References are on the website, Transport Canada and widola
Correction#3 Design and development The Puma was originally called Pluto by Bortolanza when he first designed it in the mid-1980s as an Ultralight with 990lbs max takeoff weight. Later it was renamed as the Drakken (Swedish for "dragon"). In 2008 BDC Aero Industrie redesign the aircraft according to the LAMAC regulation to fit the Advanced Ultralight Regulation at 1230lbs max takeoff weight. In 2012 BDC Aero Industrie complete the first Limited Class Category with Transport Canada where the size, structure, production procedure, and quality control were implemented to meet the standards for a max takeoff weight of 1320lbs on wheels and 1420lbs on floats. Although the airplane resemble the Italian made, the new PUMA, it has a total new structure, components and interior, and it is engineer to have a max gross weight of 1320lbs and 1420lbs on floats, as well as new engines power and configuration. Today the Puma comes with Rotax 912 UL, 912ULS, 912iS, 914UL all of them mounted on a dyno focal engine mount and no longer bed engine mount. The aircraft is made with an aluminum wing and composite fuselage. Its 28 ft (8.5 m) span wing has an area of 124 sq ft (11.5 m2) and flaps.The Puma is approved by Transport Canada as an Advanced Ultralight and Limited Class, but, as of September 2015, does not appear on the Federal Aviation Administration light-sport aircraft list References are on the website, transport canada, FAA, and widola
Correction #4 Operational history In September 2015 there total 6 Pumas made, were five Pumas registered with Transport Canada, four Advanced Ultralight, one Limited Class, and one LSA all built by BDC between 2010 and 2013. There is one Puma LSA registered in the United States with the Federal Aviation Administration in 2013 References are on Transport Canada
Correction #5 Specifications (BDC Puma) should be change to Specification Puma Aircraft General characteristics Crew: one Capacity: one passenger Length: 20.8 ft (6.3 m) Wingspan: 28 ft 0 in (8.53 m) Wing area: 124 sq ft (11.5 m2) Airfoil: Modified NACA 4412 Empty weight: 662 lb (300 kg) Gross weight: 1,232 lb (559 kg) Fuel capacity: 24 U.S. gallons (91 L; 20 imp gal) Powerplant: 1 × Rotax 912UL four cylinder, liquid and air-cooled, four stroke aircraft engine, 80 hp (60 kW) Propellers: 2-bladed, 5 ft 9 in (1.76 m) diameter Performance Maximum speed: 138 mph; 222 km/h (120 kn) at sea level Cruising speed: 132 mph; 213 km/h (115 kn) Stall speed: 43 mph; 69 km/h (37 kn) @max gross weight and full flap Never exceed speed: 161 mph; 259 km/h (140 kn) Range: 575 mi; 926 km (500 nmi) Service ceiling: 12,000 ft (3,658 m) G limits: +4g/-2g Maximum glide ratio: 11.1 Rate of climb: 900 ft/min (4.6 m/s) Rate of sink: 350 ft/min (1.8 m/s) Wing loading: 9.9 lb/sq ft (48 kg/m2) Avionics Analog and digital
References are on the websiteBAI73 (talk) 01:19, 3 November 2015 (UTC)
- As I noted above this discussion being conducted at: Talk:BDC Aero Industrie and Talk:BDC Aero Puma. Please discuss over there. - Ahunt (talk) 01:27, 3 November 2015 (UTC)